Python mach2tas Examples

Example #1

File: test_airspeed.py Project: khorton/AeroCalc_Package

    def test_03(self):

        # Mach 1, mph, 10,000 ft

        Value = A.mach2tas(1, speed_units='mph', altitude=10000)

        # truth value from NASA RP 1046

        Truth = 734.58
        self.assertTrue(RE(Value, Truth) <= 1e-5)

Example #2

File: test_airspeed.py Project: khorton/AeroCalc_Package

    def test_02(self):

        # Mach .5

        Value = A.mach2tas(.5, 59, speed_units='mph', temp_units='F')

        # truth value from NASA RP 1046

        Truth = 761.22 / 2
        self.assertTrue(RE(Value, Truth) <= 1e-5)

Example #3

File: test_airspeed.py Project: khorton/AeroCalc_Package

    def test_01(self):

        # Mach 1

        Value = A.mach2tas(1, 15)

        # truth value from NASA RP 1046

        Truth = 661.48
        self.assertTrue(RE(Value, Truth) <= 1e-5)

Example #4

File: test_airspeed.py Project: briandwendt/AeroCalc_Package

    def test_03(self):

        # Mach 1, mph, 10,000 ft

        Value = A.mach2tas(1, speed_units='mph', altitude=10000)

        # truth value from NASA RP 1046

        Truth = 734.58
        self.failUnless(RE(Value, Truth) <= 1e-5)

Example #5

File: test_airspeed.py Project: briandwendt/AeroCalc_Package

    def test_02(self):

        # Mach .5

        Value = A.mach2tas(.5, 59, speed_units='mph', temp_units='F')

        # truth value from NASA RP 1046

        Truth = 761.22 / 2
        self.failUnless(RE(Value, Truth) <= 1e-5)

Example #6

File: test_airspeed.py Project: briandwendt/AeroCalc_Package

    def test_01(self):

        # Mach 1

        Value = A.mach2tas(1, 15)

        # truth value from NASA RP 1046

        Truth = 661.48
        self.failUnless(RE(Value, Truth) <= 1e-5)